View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66370U 26145.54352316 +.00000000 +00000-0 +56600-3 0 00002
2 66370 53.1589 233.2085 0001707 83.9526 276.1670 15.30212837 07
| Epoch (UTC): | 25 May 2026 13:02:40 |
| Eccentricity: | 0.0001707 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.2085° |
| argument of perigee: | 83.9526° |
| revolutions per day: | 15.30212837 |
| mean anomaly at epoch: | 276.1670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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